Boeing 767-300
Service difficulty reports · 2,161
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '767300' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '767300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HALA0600680Pressure Switch · unknownETOPS SIGNIFICANT SYSTEM, LOW PRESS LIGHT ILLUM EICAS MSG DISPLAYED C HYD PRIM1. EICAS MSG C HYD SYS MAINT WAS NOT DISPLAYED. OPS CK CENTER HYD SYS COULD NOT DUPLICATE PROBLEM. REPLACED C1 ELECTRIC HYD PUMP PRESSURE SWITCH IAW MM 29-11-18. OPS AND LEAK CK OK SDR HALA0600674Vent Line · damagedETOPS SIGNIFICANT SYSTEM, FOUND HOLE IN NR 3 BEARING OIL VENT TUBE ON NR 2 ENGINE. REMOVED TUBE FOR EVALUATION, REMOVED AND REPLACED LINE PER POWERPLANT BUILD UP MANUAL , MM CHAP 71-00-00 LINE SECURED AND SAFETIED. LEAK CHECKED GOOD.SDR HALA0600672Panel · openBTB -WHILE TAXING OUT ROW 29 CEG, O2 PANEL FELL OUT, RTN TO GATE FOR MNT.//RESET DOOR LATCH PER AMM 35-21-15 SECURITY GOOD.SDR HALA0600667Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - RT ENG EEC MODE AMBER EICAS MSG CAME ON NEAR TOP OF CLIMB. SUCCESSFUL RESET FOLLOWING QRH PROCEDURE. T/S PER FIM 73-21-00, FOUND P5 LINE FAULT CHA/B ON PIMU. INSPECTED PHEUMATIC LINES P5 AND P2, NO DISCREPANCIES FOUND. CLEARED PISDR HALA0600666Warning Message · false activationETOPS SIGNIFICANT SYSTEM - `RUDDER RATIO` MAINTENANCE MESSAGE ON ECS/MSG EICAS PAGE. DID BITE CHECK FOR LT/RT RUDDER RATIO CONTROL/MODULE BOXES IN E&E COMPARTMENT. NO FAULTS FOUND, RESET C/W ON BOTH LT & RT BOXES MESSAGE CLEARED.SDR HALA0600768Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 8, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 PER SRM 53-00-01-2R-8, SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,SDR HALA0600759Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1074 BETWEEN 3R AND 4R. DRILLED OUT DAMAGE O A DIA OF .127 INCH PER SRM 03-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFCL INSPECTED REWORK AREA IAW D634T301, PT6, 51-00-16, NO CSDR HAL0600763Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1133 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8, SEC1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.8. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,51-00-SDR HALA0600761Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1110 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO DIA OF .128 INCH PER SRM 53-00-01-2R-8, SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-8. REWORK AREA IAW D634T301, PT6, 51-00-16, NO CRACKS NOTESDR HALA0600763Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1133, BETWEEN STR 5R AND STR 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, SDR HALA0600764Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1145 BETWEEN STR 5R AND STR 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP NO CRACKS NOTED IAW 767 NDT, PT6 51-00-19. SDR HALA0600769Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 27, BETWEEN STR 7R & STR. 8R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SRC1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PTSDR HALA0600767Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1192, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,SDR HALA0600770Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 +38. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS FREE OF CRACKS, PER STEP 3,B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767NDT, PT6, 51-00-19. QC VERISDR HALA0600772Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 + 86, BETWEEN STR 8R AND STR 9R. DRILLED OUT DAMAGE TO A DIA OF .128 INCH PER SRM 53-00-01/201 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, 51-00-19SDR HALA0600771Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1197 +78, BETWEEN STR 8R AND STR 9R. DRILL OUT DAMAGE TO A DIA OF .128 INCH PER SRM 53-00-01/201 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS FREE OF CRACKS. HFEC INSP OF HOLE, NO CRACKS NOTED IAW 767 NDT, PT6,51-00SDR HALA0600766Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1183, BETWEEN STR 6R AND STR 7R. DRILLED OUT DAMAGE TO A DIA OF .185 INCH PER SRM 53-00-01-2R-9 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B.HFEC INSP. HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, SDR HALA0600760Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1096, BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF.185 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3-B. HFEC INSPECTED REWORK AREA IAW D634T301 PT6 51-00-16, NOSDR HALA0600765Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1155 BETWEEN STR 6R AND 7R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8 SEC 1 STEP 3-A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3.B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT, PT6, 51-0SDR HALA0600762Skin · damagedLIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1126 BETWEEN STR 5R AND 6R. DRILLED OUT DAMAGE TO A DIA OF .127 INCH PER SRM 53-00-01-2R-8, SEC 1 STEP 3A. NDI TO VERIFY HOLE IS CRACK FREE PER STEP 3B. HFEC INSP HOLE, NO CRACKS NOTED IAW 767 NDT PT6, 51-00-SDR HALA0600668Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE SLOW TO START STARTER CUT OUT AT APPROX 47%, 130 SECONDS FROM FUEL ON TO IDLE SPEED. RAN NR 2 ENGINE ON GROUND, STARTER CUTOUT AT 49%, 85 SEC FROM FUEL ONTO IDLE SPEED. OK TO CONTINUE PER HAL M105 FILE 584060.SDR HALA0600665Indication Sys · erraticETOPS SIGNIFICANT SYSTEM - NR 2 EGT ERRATIC AND FLUCTUATING BETWEEN 750-350 ON CLIMBOUT FOR APPROX 2 MINS, THAN STABLE. ACCOMPLISHED FIM 77-21-00 FIG 103, NO FAULTS OR DAMAGE. CHECKED ENG WIRING PER WDM 77-21-11 AND SSM 77-00-01 SHOOK HARNESS, NO FLUCTUATIONSDR HALA0600664Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ICAS MSG R ENG EEC MODE DISPLAYED, SYS WAS SUCCESSFULLY RESET. T/S PER FIM 73-21-00 FIG 113, NO MSG IN PIMU CLEARED MTC MSG RUN ENG PER FIM PIMU INDEX 350-22. MSG DID NOT RETURN, SYS OK.SDR HALA0600670Hydraulic System · unknownETOPS SIGNIFICANT SYSTEM - DURING CLIMBOUT DURING THE LAST 10,000FT OF CLIMB L ENG PRIMARY HYD PRESS LIGHT CAME ON FOLLOWED BY THE L ELECT DEMAND PRESS LT. CREW NOTED PRESS WOULD DROP TO APPX 1700 PSI, RTN TO NORMAL & PRESS LIGHT WENT OUT. HYD QUANTITY 1.4 ISDR HALA0600669Idg · malfunctionedETOPS SIGNIFICANT SYSTEM - ON BASE LEG LANDING IN HNL RECEIVED L GEN OFF LIGHT & BOTH UTILITY BUSS OFF LIGHTS. STARTED THE APU, LANDED THEN RESET GEN CONT SWITCH. CONDITION RETURNED TO NORMAL. PERFORMED BPCU BITE PROCEDURE PER FIM 24-20-00-MSG FOR LT SYS ARSDR HALA0600671Status Message · false activationETOPS SIGNIFICANT SYSTEM - WXR SYS STATUS LIGHT CAME ON. RADAR OPS NORMAL. RESET WEATHER RADAR SYSTEM. OPS GOOD CHECK PER M/M 34-43-00.SDR HALA0600653Eec · faultedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE EEC MODE EICAS MESSAGE DISPLAYED. T/S PER FIM 73-21-00 FIG 113 PIMU FAULTED EEC CHANNEL A/B P2 AND P5 LINE. INSPECTED P2 AND P5 LINES PER FIM 350-21. NO FAULTS NOTED. CLEARED PIMU AND RAN ENG NR 2 TO 1.4 EPR. CONFIRSDR NOCA12906Blades · bird strikeBIRD STIRKE ON TAKE OFF FROM BJL RT ENGINE, FAN VIB 4.1 RECORDED. LANDED SAFELY AT BJL AFTER FUEL DUMPED. REPLACED 4 FAN BALDES, OPS NORMAL.SDR HALA0600656Wire · damagedETOPS SIGNIFICANT SYSTEM - CALLS ON ANY RADIO FAILED TO DISPLAY SELCAL MESSAGE AND SOUND CHIME. REPAIRED WIRING TO SELCAL CODING OPS CHECK OK PER AMM 23-21-00.SDR HALA0600655Warning Light · illuminatedETOPS SIGNIFICANT SYSTEM - (LOWER EICAS) STATUS MSG -WXR SYS-. BOTH LEFT & RIGHT WX RADAR SYSTEMS OPS CHECK OK PER AMM 34-43-00. NO FAULTS FOUND.SDR HALA0600657Wire · failedETOPS SIGNIFICANT SYSTEM - BOTH FMCS FAIL WHEN RIGHT EFI SWITCH SELECTED TO ALTN. REPAIRED WIRING TO RELAY K2070 FMC NR 1 & NR 2, OPS CHECK OK PER AMM 34-61-00. EFIS SYSTEM OPS CHECK OK PER AMM 34-22-00.SDR HALA0600688Support Bracket · crackedLT WING T/E WS 530 LWR T/E PANEL SUPPORT BRACKET CRACKED IN RADUS OB SIDE OF IB AILERON OB SUPPORT FITTING. ACCESSED LOWER T/E PANEL FASTENERS AND REMOVED CRACKED BRACKET JUST OB OF AILERON SUPPORT FITTING. FABRICATED REPLACEMENT BRACKET FROM 7075-0 BARE SHEESDR HALA0600654Shutoff Valve · failedBTB - NR 1 ENGINE NO BLEED AIR. T/S PER FIM - PNEUMATIC SUPPLY BITE MODULE FAULTED LEFT ENG PRSOV. REMOVED AND REPLACED LEFT ENG PRSOV PER M/M 36-11-09. ALSO REPLACED LEFT ENG BLEED SUPPLY CONTROL CARD IN P50 PANEL PER MM 36-11-12. RAN ENGINE AND PRSOV OP SDR HALA0600719Support · damagedRT WING T/E, AFT PANEL SUPPORT FOR PNL NR 661 IB AFT L ANGLE HAS A FIGURE 8 HOLE AND LWR FASTENER LOOSE. REMOVED, FABRICATED NEW AND INSTALLED L ANGLE RT WING T/E AFT PANEL SUPPORT IAW OHM 20-50-01-06-0, MM 51-21-00-377-001.SDR HALA0600718Channel · crackedR/W CRACKED CHANNEL IB END OB FLAP 7 INCHES FROM L/E OF CLOSE OUT PANEL. REMOVED CRACKED CHANNEL FROM R/W IB END OF OB FLAP IAW SRM 51-40-02.REPAIRED CHANNEL IAW SRM 51-70-11 FIG 1 STEPS 1-12. REPAIRED DOUBLER MATERIAL 2024-T3 .63 INCHES, LOT NR 709033. INSTASDR HALA0600687Crank Assy · chafedR/W OB FLAP ACTUATOR CRANK ARM 6-9 LINK LWR OB SIDE CHAFING ON LINK SUPPORT FITTING AT FWD OB SIDE. REPAIRED CHAFED AREA ON LINK SUPPOR AND 6-9 LINK IAW SRM 57-53-02 AND SRM 51-20-06.SDR UPS06647908Brake · leakingINSPECTION TYPE: ETOP RT HYDRAULIC QTY ZERO; EICAS MSG RT HYD QTY DISPLAYED. SYSTEM PRESSURE LIGHT NOT ILLUM. NOTED AFTER EXITING RUNWAY ON LANDING. FOUND DAMAGE TO NR 8 BRAKE (RT AFT OB). THIS FLIGHT INVOLVED A BRAKE ROTOR FAILURE LEADING TO THE COMPLETE LOSSDR HALA0600717Rib · crackedANGLE CRACKED IN FIXED L/E FWD OF RIB ON OB SIDE OF NR 8 SLAT, OB ROTARY ACTUATOR. REMOVED ANGLE IN L/E OB NR 8 ROTARY ACTUATOR, REPLACED ANGLE AND INSTALLED ALL BUT (3) RIVETS, COMMON TO SKIN IAW SRM 51-40-01. INSTALLED (3) FASTNERS COMMON TO L/E SKIN IAW SSDR UPS06647836Servo · malfunctionedUNCOMMANDED RUDDER YAW TWICE IN FLIGHT. R & R LT & RT YAW DAMPER SERVO IAW MM 22-21-02-4. LEAK CHECK RIGHT & LEFT YAW DAMPER SERVO PER TECH SERVICES. R&R RIGHT YAW DAMPER MODULE ASSY IAW MM 22-21-04-2. ALSO R&R LEFT YAW DAMPER MODULE ASSY AS PRECAUTIONARY. PSDR HALA0600643Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, EICAS STATUS MESSAGE "ELEVATOR FEEL" DISPLAYED. ACCOMPLISHED FIM 27-30-00 FIG 106, NO DEFECTS NOTED.SDR HALA0600646Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, APU BITE BITE EICAS MTC MSG FOUND ON OVERNIGHT CHECK. PERFORMED APU ECU BITE PER FIM 49-11-00/101 FIG 103, NO FAULTS ERASED. MSG ON EICAS ECS MSG PAGE DID NOT RETURN.SDR HALA0600645Warning Message · false indicationETOPS SIGNIFICANT SYSTEM, L ENG FIRE LP2 STATUS MSG FOUND ON OVERNIGHT CHECK. PERFORMED TEST PER FIM 26-11-00/101 FIG 104, NO FAULTS FOUND MSGV DID NOT RETURN.SDR HALA0600647Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM, FMC DISPLAYED ON EICAS WITH NO CORRESPONDING FMS MESSAGE. NO EICAS MESSAGE "FMC" DISPLAYED ON ARRIVAL. OPS CHECK OK PER MM 34-61-00.SDR HALA0600747Keelbeam · corrodedCORROSION ON KEELBEAM SURFACE, BS 970, RBL 8. REMOVED CORROSION ON KEEL BEAM OF BS 970 RBL 8 IN AN AREAS OF 2.5 X 1.5 X .035 INCH FROM ORIGINAL THICKNESS OF .360 INCH. FOUND BLENDED AREA TO BE IN LIMITS PER SRM 53-50-12 FIGURE 101.SDR HALA0600642A/C Pack · inoperativeETOPS SIGNIFICANT SYSTEM - R PACK INOP LT ON DURING DESCENT. R PACK BITE MSG ON MAINT MESSAGE DISPLAYED ON EICAS. PERFORMED FIM 21-51-00 FIG 103. RT PACK TEMP CONT INDICATED TEMP VALVE FAULT. CLEANED CONNECTOR ON VALVE. RT PACK OPS NORMAL PER FIM 21-51-00SDR HALA0600639Control Column · disconnectedBTB -COLUMN DISC- ALERT MSG CAME ON DURING TAXI. PERFORMED FIM 27-30-00 AND COLUMN WAS PHYSICALLY DISCONNECTED. RECONNECTED CONTROL COLUMN PER AMM 27-31-10, OPS CHECK GOOD, MSG CLEARED.SDR HALA0600686Seal · damagedBLADE SEAL DAMAGED ON LEADING EDGE ON NR 2 ENGINE PYLON PANEL NR 441AT. REMOVED RIVETS FROM NR 2 ENG PYLON PANEL NR 441 AT BLADE SEAL IAW SRM 51-40-02.SDR HALA0600685Attach Fitting · crackedIB T-CLIP IS CRACKED ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY, NAS STATION 308. REMOVED AND REPLACED T-CLIP ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY NAC, STA 308. IAW SRM 51-40-02.SDR HALA0600635Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - ELEV FELL LIGHT ILLUMINATED DURING APPROACH WITH ELEV FELL EICAS MESSAGE. ACCOMPLISHED FIM 27-30-06 FIG 106, NO DEFECTS NOTED, SYS TEST OK.SDR HALA0600633Skin · scratchedON WALKAROUND FOUND SCRATCH 30 INCHES BELOW AFT EDGE OF L-4 DOOR. BLENDED AREA, PERFORMED FLOOR PENETRANT TEST, NO CRACKS NOTED. TREATED, PRIMED & PAINTED AREAS PER SRM. DAMAGE OF SCRATCH WITHIN LIMITS PER SRM 53-00-01/101, SILVER DOT INSTALLED. OK FOR SER
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